WO2013017789A3 - Device for supplying an aircraft on the ground with electricity - Google Patents

Device for supplying an aircraft on the ground with electricity Download PDF

Info

Publication number
WO2013017789A3
WO2013017789A3 PCT/FR2012/051790 FR2012051790W WO2013017789A3 WO 2013017789 A3 WO2013017789 A3 WO 2013017789A3 FR 2012051790 W FR2012051790 W FR 2012051790W WO 2013017789 A3 WO2013017789 A3 WO 2013017789A3
Authority
WO
WIPO (PCT)
Prior art keywords
network
aircraft
supplying
electricity
ground
Prior art date
Application number
PCT/FR2012/051790
Other languages
French (fr)
Other versions
WO2013017789A2 (en
Inventor
Sébastien VIEILLARD
Serge Berenger
Serge Thierry ROQUES
Pascal Dauriac
Original Assignee
Hispano-Suiza
Turbomeca
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hispano-Suiza, Turbomeca filed Critical Hispano-Suiza
Priority to US14/234,541 priority Critical patent/US9592907B2/en
Priority to BR112014001457-4A priority patent/BR112014001457B1/en
Priority to CN201280035443.3A priority patent/CN103703649B/en
Priority to CA2842086A priority patent/CA2842086C/en
Priority to RU2014108158/07A priority patent/RU2603693C2/en
Priority to ES12753762.9T priority patent/ES2554950T3/en
Priority to EP12753762.9A priority patent/EP2740191B1/en
Priority to JP2014523366A priority patent/JP5955960B2/en
Publication of WO2013017789A2 publication Critical patent/WO2013017789A2/en
Publication of WO2013017789A3 publication Critical patent/WO2013017789A3/en

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00—Circuit arrangements for mains or distribution networks not specified as ac or dc
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/405—Powered wheels, e.g. for taxing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
    • H02J9/04—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
    • H02J9/06—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40—The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Control Of Eletrric Generators (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
  • Direct Current Feeding And Distribution (AREA)
  • Synchronous Machinery (AREA)
  • Stand-By Power Supply Arrangements (AREA)

Abstract

The invention relates to a device (210) for supplying an aircraft on the ground with electricity, comprising two electric generators (216, 218) driven by an auxiliary power unit (220), characterized in that the first generator is connected by connection/disconnection means (232) to an aircraft network (212) and to an electrical taxiing network (214), so as to either provide an AC voltage Vac2 to the aircraft network when it is connected to this network, or to provide an AC voltage Vac1 or power P to the taxiing network when it is connected to this network, and in that the second generator is connected by connection/disconnection means (232) to the aircraft network (212) so as to provide this network with an AC voltage Vac2 only when the first generator is supplying the taxiing network.
PCT/FR2012/051790 2011-08-04 2012-07-27 Device for supplying an aircraft on the ground with electricity WO2013017789A2 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US14/234,541 US9592907B2 (en) 2011-08-04 2012-07-27 Device for electrically powering an aircraft on the ground
BR112014001457-4A BR112014001457B1 (en) 2011-08-04 2012-07-27 ground aircraft power supply device
CN201280035443.3A CN103703649B (en) 2011-08-04 2012-07-27 A kind of equipment for powering for airborne vehicle on the ground
CA2842086A CA2842086C (en) 2011-08-04 2012-07-27 Device for supplying an aircraft on the ground with electricity
RU2014108158/07A RU2603693C2 (en) 2011-08-04 2012-07-27 Device for electrically powering an aircraft on the ground
ES12753762.9T ES2554950T3 (en) 2011-08-04 2012-07-27 Power supply device of an aircraft on the ground
EP12753762.9A EP2740191B1 (en) 2011-08-04 2012-07-27 Device for supplying an aircraft on the ground with electricity
JP2014523366A JP5955960B2 (en) 2011-08-04 2012-07-27 Equipment for supplying power to ground aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1157169A FR2978878B1 (en) 2011-08-04 2011-08-04 DEVICE FOR ELECTRICALLY SUPPLYING AN AIRCRAFT TO THE GROUND.
FR1157169 2011-08-04

Publications (2)

Publication Number Publication Date
WO2013017789A2 WO2013017789A2 (en) 2013-02-07
WO2013017789A3 true WO2013017789A3 (en) 2013-10-24

Family

ID=46785751

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2012/051790 WO2013017789A2 (en) 2011-08-04 2012-07-27 Device for supplying an aircraft on the ground with electricity

Country Status (10)

Country Link
US (1) US9592907B2 (en)
EP (1) EP2740191B1 (en)
JP (1) JP5955960B2 (en)
CN (1) CN103703649B (en)
BR (1) BR112014001457B1 (en)
CA (1) CA2842086C (en)
ES (1) ES2554950T3 (en)
FR (1) FR2978878B1 (en)
RU (1) RU2603693C2 (en)
WO (1) WO2013017789A2 (en)

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FR2988694B1 (en) * 2012-03-30 2014-03-28 Hispano Suiza Sa DEVICE FOR ELECTRICALLY SUPPLYING AN AIRCRAFT ON THE GROUND
CN103746448A (en) * 2013-12-04 2014-04-23 中国飞行试验研究院 Y-7 airplane power supply system
US20150283908A1 (en) * 2014-04-02 2015-10-08 Hamilton Sundstrand Corporation Systems utilizing a controllable voltage ac generator system
EP3095988A1 (en) * 2015-05-18 2016-11-23 Airbus Operations, S.L. Auxiliary power unit starting system for an aircraft
GB201511033D0 (en) * 2015-05-19 2015-08-05 Rolls Royce Plc Aircraft electrical network
US9771149B2 (en) * 2015-10-30 2017-09-26 Honeywell International Inc. Gate departure system for aircraft
EP3235723B1 (en) * 2016-04-22 2019-11-27 Rolls-Royce plc Aircraft electrical network
FR3054738B1 (en) 2016-07-29 2020-10-23 Airbus Helicopters ELECTRICAL ARCHITECTURE WITH DOUBLE SECONDARY ELECTRICAL NETWORK FOR STARTING AIRCRAFT ENGINES
GB201715598D0 (en) 2017-09-27 2017-11-08 Rolls Royce Plc Electrical interconnect system
RU2684971C1 (en) * 2017-12-13 2019-04-16 Эйрбас Хеликоптерс Electrical system with double secondary electric mains for starting aircraft engines
FR3079820B1 (en) * 2018-04-09 2020-04-17 Safran Electrical & Power STARTING / GENERATION SYSTEM AND METHOD FOR AIRCRAFT TURBOMACHINE
FR3087960B1 (en) * 2018-10-31 2021-06-04 Safran ELECTRICAL ENERGY CONVERSION AND TRANSPORT SYSTEM FOR THE INTERNAL HYBRIDATION OF A TURBOREACTOR AIRCRAFT
EP3931097A4 (en) 2019-03-01 2022-11-16 Pratt & Whitney Canada Corp. Degraded mode operation of hybrid electric propulsion systems
WO2020180381A1 (en) 2019-03-01 2020-09-10 United Technologies Advanced Projects, Inc. Indicators for hybrid electrical powerplants
EP3931098A4 (en) 2019-03-01 2022-11-16 Pratt & Whitney Canada Corp. Normal mode operation of hybrid electric propulsion systems
WO2020219111A1 (en) 2019-04-25 2020-10-29 United Technologies Corporation Control systems for hybrid electric powerplants
US11794917B2 (en) 2020-05-15 2023-10-24 Pratt & Whitney Canada Corp. Parallel control loops for hybrid electric aircraft
US11958622B2 (en) 2020-05-15 2024-04-16 Pratt & Whitney Canada Corp. Protection functions

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EP1897804A2 (en) * 2006-09-07 2008-03-12 The Boeing Company Systems and methods for controlling aricraft electrical power
WO2009125007A2 (en) * 2008-04-09 2009-10-15 Thales Method for managing electrical network
EP2236419A2 (en) * 2009-04-01 2010-10-06 Rolls-Royce plc An apparatus for taxiing an aircraft
FR2954283A1 (en) * 2009-12-23 2011-06-24 Hispano Suiza Sa AIRCRAFT COMPRISING AN ELECTRICAL STARTER-GENERATOR FOR THE OR TURBOREACTOR AND A CLEARING TRAIN EQUIPPED WITH AN ELECTRIC ENGINE OF MANEUVER ON THE GROUND

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EP1897804A2 (en) * 2006-09-07 2008-03-12 The Boeing Company Systems and methods for controlling aricraft electrical power
WO2009125007A2 (en) * 2008-04-09 2009-10-15 Thales Method for managing electrical network
EP2236419A2 (en) * 2009-04-01 2010-10-06 Rolls-Royce plc An apparatus for taxiing an aircraft
FR2954283A1 (en) * 2009-12-23 2011-06-24 Hispano Suiza Sa AIRCRAFT COMPRISING AN ELECTRICAL STARTER-GENERATOR FOR THE OR TURBOREACTOR AND A CLEARING TRAIN EQUIPPED WITH AN ELECTRIC ENGINE OF MANEUVER ON THE GROUND

Also Published As

Publication number Publication date
WO2013017789A2 (en) 2013-02-07
CA2842086C (en) 2019-05-14
US20140138479A1 (en) 2014-05-22
US9592907B2 (en) 2017-03-14
BR112014001457A2 (en) 2018-08-14
ES2554950T3 (en) 2015-12-28
CA2842086A1 (en) 2013-02-07
JP5955960B2 (en) 2016-07-20
BR112014001457B1 (en) 2021-05-25
FR2978878B1 (en) 2013-08-09
CN103703649B (en) 2016-08-31
FR2978878A1 (en) 2013-02-08
JP2014525873A (en) 2014-10-02
RU2014108158A (en) 2015-09-10
EP2740191A2 (en) 2014-06-11
CN103703649A (en) 2014-04-02
RU2603693C2 (en) 2016-11-27
EP2740191B1 (en) 2015-10-07

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